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Enhancement of heat transfer in a synthetic jet actuated by piston cylinder
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Modern electronics demand more powerful cooling systems due to an increase in heat dissipation. The traditional cooling techniques reached their limit and the synthetic jet impingement arises as a promising method for cooling of modern electronic systems. This paper presents the experimental studies on the heat transfer characteristics of a synthetic jet. The synthetic jet is driven by a piston actuator. The effects of dimensionless parameters like the distance between the orifice and heater plate (Z/D), the ratio of stroke length to diameter of orifice ( L/D), Stokes number, and Reynolds number are discussed. The effect of orifice geometry, number of orifices are also presented. The results indicate that the Z/D and Stokes number have a significant influence on the heat transfer rate. As the Stokes number increases the heat transfer increases due to an increase in axial momentum and turbulence in the flow direction. For circular orifice and at high Z/D, the L/D ratio should be higher for better heat transfer. Rectangular orifice performs better than square and circular geometries. When compared to single jet multiple jets have a higher heat transfer rate. Maximum and minimum values of normalized pressure ( Pnr) are achieved for high Stokes number and smaller areas of the orifice.
Title: Enhancement of heat transfer in a synthetic jet actuated by piston cylinder
Description:
Modern electronics demand more powerful cooling systems due to an increase in heat dissipation.
The traditional cooling techniques reached their limit and the synthetic jet impingement arises as a promising method for cooling of modern electronic systems.
This paper presents the experimental studies on the heat transfer characteristics of a synthetic jet.
The synthetic jet is driven by a piston actuator.
The effects of dimensionless parameters like the distance between the orifice and heater plate (Z/D), the ratio of stroke length to diameter of orifice ( L/D), Stokes number, and Reynolds number are discussed.
The effect of orifice geometry, number of orifices are also presented.
The results indicate that the Z/D and Stokes number have a significant influence on the heat transfer rate.
As the Stokes number increases the heat transfer increases due to an increase in axial momentum and turbulence in the flow direction.
For circular orifice and at high Z/D, the L/D ratio should be higher for better heat transfer.
Rectangular orifice performs better than square and circular geometries.
When compared to single jet multiple jets have a higher heat transfer rate.
Maximum and minimum values of normalized pressure ( Pnr) are achieved for high Stokes number and smaller areas of the orifice.
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